STC SA4201NM-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA4201NM-D Certificate This certificate issued to: Hollingsead International SURRENDERED 2226 Goodyear Avenue Ventura, California 93003 on 60-18-09 Part 25 of the Federal Aviation Regulations.

Original Product Type Certificate Number 4A25 Make: McDONNELL DOUGLAS Model: DC-8-62, -63 Description of Type Design Change:

o Installation of engine driven hydraulic pumps in accordance with Air Transport International documentation: Drawing 29-DC8-15, Rev. A Dated 11/26/91, or later FAA approved revision.

Limitations and Conditions: This approval should not be incorporated on any certificated product of this model on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated modifications will not introduce any adverse effect upon the airworthiness of the certificated product. A copy of this STC must be included in the permanent records of the modified aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of Application: November 27, 1991 Date of Issuance: January 8, 1992

SEAL AVIOL

TOMANSTRAND Date Reissued: April 12, 1995; December 16, 1996;

April 1, 1998; August 1, 2005; May 7, 2007 Date Amended:

By Direction of the Administrator Calt K. Woo (Signature) Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office (Title)

TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street) (City, State, and Zip code) trom (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):